View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 16986U 26018.21737462 +.00000000 +00000-0 +36773-3 0 00001
2 16986 82.5281 289.3919 0007803 39.3704 320.8103 15.32037902 02
| Epoch (UTC): | 18 January 2026 05:13:01 |
| Eccentricity: | 0.0007803 |
| inclination: | 82.5281° |
| perigee height: | 464 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 289.3919° |
| argument of perigee: | 39.3704° |
| revolutions per day: | 15.32037902 |
| mean anomaly at epoch: | 320.8103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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